JP3308346B2 - Air probe pin board for board inspection equipment - Google Patents

Air probe pin board for board inspection equipment

Info

Publication number
JP3308346B2
JP3308346B2 JP16425293A JP16425293A JP3308346B2 JP 3308346 B2 JP3308346 B2 JP 3308346B2 JP 16425293 A JP16425293 A JP 16425293A JP 16425293 A JP16425293 A JP 16425293A JP 3308346 B2 JP3308346 B2 JP 3308346B2
Authority
JP
Japan
Prior art keywords
air
diameter portion
probe
small
diameter
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
JP16425293A
Other languages
Japanese (ja)
Other versions
JPH06347477A (en
Inventor
和彦 富山
司 和田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hioki EE Corp
Original Assignee
Hioki EE Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hioki EE Corp filed Critical Hioki EE Corp
Priority to JP16425293A priority Critical patent/JP3308346B2/en
Publication of JPH06347477A publication Critical patent/JPH06347477A/en
Application granted granted Critical
Publication of JP3308346B2 publication Critical patent/JP3308346B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明はインサーキットテスタ
ー、ファンクションテスター等の基板検査装置用の複数
のプローブを立設した支持体からなるピンボードに関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a pin board comprising a support on which a plurality of probes are erected for a board inspection apparatus such as an in-circuit tester and a function tester.

【0002】[0002]

【従来の技術】従来、実装基板即ち多数の電子部品を半
田付けしたプリント基板はインサーキットテスターを用
い、その基板の必要な各測定点にプローブの先端を接触
して、各部品の電気的測定によって基板の良否の判定を
行っている。このようなインサーキットテスターには種
々のものがあるが、プレス式では測定に際し、図11に
示すような検査治具たる複数のプローブ10を立設した
樹脂製の支持体12からなるピンボード14を用い、実
装基板16をそのピンボード14の上に載せ、上方から
矢印方向にプレスして固定する。すると、各プローブ1
0は基板16に押されて縮み、先端がそのストローク
(後退量)に比例した接触圧で、基板16に実装された
電子部品の電極やそこに設けられているパターン等の測
定点と電気的に接続する。なお、各プローブ10は例え
ばプランジャ18、バレル20、圧縮スプリング、リー
ド線22等からなり、そのプランジャ18にはバレル2
0の内部に収納されている圧縮スプリングにより突出方
向(上方)にスプリング力が作用するため、プランジャ
18がバレル20の内部を摺動可能になっている。又、
各プローブ10の立設に際しては支持体12の適切な位
置にそれぞれ貫通孔を開け、そこに挿通して固定する。
又、基板16は水平方向に移動しないように固定する。
2. Description of the Related Art Conventionally, a mounting substrate, that is, a printed circuit board on which a large number of electronic components are soldered, uses an in-circuit tester, and the tip of a probe is brought into contact with each required measuring point on the substrate to perform electrical measurement of each component. Is used to determine the quality of the substrate. There are various types of such in-circuit testers. In the case of the press type, when performing measurement, a pin board 14 made of a resin support 12 having a plurality of probes 10 erected as inspection jigs as shown in FIG. Then, the mounting substrate 16 is placed on the pin board 14 and fixed by pressing in the direction of the arrow from above. Then, each probe 1
The reference numeral 0 denotes a contact pressure proportional to the stroke (retraction amount) of the electronic component mounted on the substrate 16 and a measurement point of a pattern or the like provided on the electrode, which is in contact with the measuring point of the electronic component mounted on the substrate 16. Connect to Each probe 10 includes, for example, a plunger 18, a barrel 20, a compression spring, a lead wire 22, and the like.
Since the spring force acts in the protruding direction (upward) by the compression spring housed in the inside of the barrel 0, the plunger 18 can slide inside the barrel 20. or,
When each probe 10 is erected, a through hole is opened at an appropriate position on the support 12 and inserted into the through hole and fixed.
The substrate 16 is fixed so as not to move in the horizontal direction.

【0003】[0003]

【発明が解決しようとする課題】しかしながら、このよ
うなプローブ10付きのピンボード14を用いると、基
板16の測定点に凹凸があれば、先端が凹の測定点に接
触した時と、凸の測定点に接触した時とで同一のプロー
ブ10でもストロークが変わり、接触圧も変わる。それ
故、接触抵抗も変わって測定点の凹凸が測定結果に影響
を与えるため問題がある。しかも、基板16をプレスし
てプローブ10の先端に押し付けても、接触圧が静圧の
ため半田付け箇所にできるフラックス膜を突き破れない
場合がある。又、プローブ10は構造が複雑であり、バ
レル20にスプリングを内蔵するため、外形が太くな
り、プローブ同士を接近させても微細な測定点間のピッ
チに対応できない。
However, when such a pin board 14 with the probe 10 is used, if the measurement points on the substrate 16 have irregularities, the contact between the measurement points having the concave tip and the convex one is different. The stroke and the contact pressure of the same probe 10 change when the probe 10 comes into contact with the measurement point. Therefore, there is a problem that the contact resistance changes and the irregularities of the measurement point affect the measurement result. In addition, even when the substrate 16 is pressed and pressed against the tip of the probe 10, there is a case where the contact pressure is a static pressure, so that the flux film formed at the soldering position cannot be broken. Further, since the probe 10 has a complicated structure and a spring is built in the barrel 20, the outer shape becomes thick, and even if the probes are brought close to each other, it is impossible to cope with a fine pitch between measurement points.

【0004】本発明はこのような従来の問題点に着目し
てなされたものであり、微細なピッチにも対応可能で、
半田付け箇所のフラックス膜を破り易く、接触圧を基板
上の測定点の凹凸に関係なく一定にでき、正確な測定結
果が得易い基板検査装置用のエアプローブピンボードを
提供することを目的とする。
The present invention has been made in view of such a conventional problem, and can cope with a fine pitch.
An object of the present invention is to provide an air probe pin board for a board inspection device which can easily break a flux film at a soldering point, can maintain a constant contact pressure regardless of unevenness of a measurement point on a board, and can easily obtain an accurate measurement result. I do.

【0005】[0005]

【課題を解決するための手段】上記目的を達成するため
に、本発明による基板検査装置用のエアプローブピンボ
ード24には複数のエアプローブ26を立設した支持体
28を用いる。そして、それ等の各エアプローブ26と
して、先端側を大径部30、後端側を小径部32に形成
し、その大径部30と小径部32との間を円錐台状の段
付部38に形成して、後端に小径部32の径より拡大し
たストッパー34を備えた細長い棒状体を用い、支持体
28の内部に各エアプローブ26の中間部を収納する複
数のエアプローブ26に共通の配管連結孔50付き空気
室52を設け、その空気室52で分けられた支持体28
の一方の側部分に各エアプローブ26の大径部30より
僅かに大きな径を有する大径部挿通孔48をそれぞれ設
け、他方の側部分に各エアプローブ26の小径部32よ
り僅かに大きな径を有する小径部挿通孔54をそれぞれ
設ける
In order to achieve the above object, a support 28 having a plurality of air probes 26 erected thereon is used for an air probe pin board 24 for a substrate inspection apparatus according to the present invention. Each of the air probes 26 has a large-diameter portion 30 at the front end and a small-diameter portion 32 at the rear end, and a truncated cone-shaped stepped portion between the large-diameter portion 30 and the small-diameter portion 32. 38, and a plurality of air probes 26 that house an intermediate portion of each air probe 26 inside the support 28 using an elongated rod-shaped body provided with a stopper 34 that is larger than the diameter of the small diameter portion 32 at the rear end. An air chamber 52 having a common pipe connection hole 50 is provided, and the support 28 divided by the air chamber 52 is provided.
The large diameter portion insertion hole 48 having a diameter slightly larger than the large diameter portion 30 of each air probe 26 is provided on one side portion of the air probe 26, and the diameter slightly larger than the small diameter portion 32 of each air probe 26 is provided on the other side portion. The small-diameter portion insertion hole 54 having the

【0006】又は、支持体76の内部に各エアプローブ
74の中間部をそれぞれ収納する空気室82を設け、そ
れ等の空気室82を配管連結孔84付き空気分配孔86
を介して連結する。
Alternatively, an air chamber 82 for accommodating an intermediate portion of each air probe 74 is provided inside a support 76, and these air chambers 82 are connected to air distribution holes 86 with pipe connection holes 84.
Connect through.

【0007】[0007]

【作用】上記のように構成し、支持体28の内部に各エ
アプローブ26の中間部を収納する複数のエアプローブ
26に共通の配管連結孔50付き空気室52を設け、そ
の空気室52で分けられた支持体28の一方の側部分に
各エアプローブ26の大径部30より僅かに大きな径を
有する大径部挿通孔48をそれぞれ設け、他方の側部分
に各エアプローブ26の小径部32より僅かに大きな径
を有する小径部挿通孔54をそれぞれ設けると、圧縮空
気を配管から連結孔50を通じて空気室52の内部に供
給し、或いは空気室52から連結孔50を通じ、配管を
経て排気できる。
An air chamber 52 having a pipe connection hole 50 common to a plurality of air probes 26 accommodating an intermediate portion of each air probe 26 is provided inside the support 28, and the air chamber 52 is formed by the air chamber 52. A large-diameter portion insertion hole 48 having a diameter slightly larger than the large-diameter portion 30 of each air probe 26 is provided on one side portion of the divided support member 28, and a small-diameter portion of each air probe 26 is formed on the other side portion. When the small-diameter-portion insertion holes 54 each having a diameter slightly larger than 32 are provided, compressed air is supplied from the pipe to the inside of the air chamber 52 through the connection hole 50, or is discharged from the air chamber 52 through the connection hole 50 through the pipe. it can.

【0008】それ故、供給した圧縮空気が空気室52に
充満すると、大径部30と小径部32との間に形成した
円錐台状段付部38の斜面に圧縮空気圧が作用し、大径
部30、小径部32が共に対応する挿通孔48、54の
内部をそれぞれ摺動して先端方向に素早く突出を開始す
る。一旦、突出を開始すると圧縮空気圧は大径部30の
断面積から小径部32の断面積を除いた面積に直接作用
する。しかも、大径部30と小径部32の周囲の僅かな
隙間から圧縮空気が大気側に洩れ、プローブ26が支持
体28の内壁から浮き上がって非接触状態となる。する
と、摺動抵抗は空気層のせん断抵抗となり、無視できる
程度の微小な値となる。そこで、各エアプローブ26の
突出方向に少し離して被検査基板70を設置し、固定し
ておけば、各エアプローブ26の先端を基板70上の測
定点にそれぞれ接触できる。このような各エアプローブ
26の接触圧(静圧)は測定点の凹凸に基づくストロー
クに関係なく、供給する圧縮空気圧により定まり、各エ
アプローブ26の先端が基板70に衝突する衝突圧(動
圧)は圧縮空気の流量によって定まる。そして、各エア
プローブ26の最大突出量は後端に備えたストッパー3
4の位置により定まる。なお、空気室52から排気する
と、段付部38の斜面に吸引作用が及ぶため、各エアプ
ローブ26が素早く後退する。
Therefore, when the supplied compressed air fills the air chamber 52, compressed air pressure acts on the slope of the frustoconical stepped portion 38 formed between the large diameter portion 30 and the small diameter portion 32, and the large diameter The portion 30 and the small-diameter portion 32 slide inside the corresponding insertion holes 48 and 54, respectively, and quickly start projecting toward the distal end. Once the projection starts, the compressed air pressure acts directly on the area obtained by removing the cross-sectional area of the large-diameter portion 30 from the cross-sectional area of the small-diameter portion 32. In addition, the compressed air leaks to the atmosphere side from a small gap around the large diameter portion 30 and the small diameter portion 32, and the probe 26 floats up from the inner wall of the support member 28 to be in a non-contact state. Then, the sliding resistance becomes the shear resistance of the air layer, and has a negligible minute value. Therefore, if the substrate 70 to be inspected is set a little apart in the direction in which the air probes 26 protrude and is fixed, the tip of each air probe 26 can be brought into contact with a measurement point on the substrate 70. The contact pressure (static pressure) of each air probe 26 is determined by the supplied compressed air pressure regardless of the stroke based on the unevenness of the measurement point, and the collision pressure (dynamic pressure) at which the tip of each air probe 26 collides with the substrate 70 is used. ) Is determined by the flow rate of the compressed air. The maximum protrusion amount of each air probe 26 is determined by the stopper 3 provided at the rear end.
It is determined by the position of 4. When the air is exhausted from the air chamber 52, the suction action is exerted on the slope of the stepped portion 38, so that each air probe 26 retreats quickly.

【0009】又、支持体76の内部に各エアプローブ7
4の中間部をそれぞれ収納する空気室82を設け、それ
等の空気室82を配管連結孔84付き空気分配孔86を
介して連結すると、圧縮空気圧が作用する面積が各空気
室82と空気分配孔86の内面となって小さくなるた
め、機械的強度が大きくなる。
Each air probe 7 is provided inside the support 76.
When the air chambers 82 for accommodating the intermediate portions of the air chambers 4 are provided, and these air chambers 82 are connected to each other through the air distribution holes 86 having the pipe connection holes 84, the area where the compressed air pressure acts is equal to each air chamber 82. Since the inner surface of the hole 86 becomes smaller, the mechanical strength increases.

【0010】[0010]

【実施例】以下、添付図面に基づいて、本発明の実施例
を説明する。図1は本発明を適用したインサーキットテ
スタの測定前のエアプローブピンボードを示す縦断面
図、図2はその一点鎖線円内に対応する拡大図である。
図中、24はピンボード、26(26a、26b、26
c)はそのエアプローブ、28はそれ等のエアプローブ
26を立設した樹脂製の支持体である。これ等のエアプ
ローブ26はいずれも金属性の細長い棒状体にし、先端
側を大径部30、後端側を小径部32に形成し、後端に
大径部30の径とほぼ等しい太さのストッパー34を備
える。しかも、大径部30の端部36は円錐状に形成
し、大径部30と小径部32との間の段付部38は面取
りして円錐台状に形成する。なお、ストッパー34には
リード線(図示なし)を接続する。このように、各エア
プローブ26を細長い棒状体にすると、先端同士を互い
に至近距離に近付けることができるため、微細ピッチに
対応可能になる。又、支持体28は2枚の方形状平板4
0、42を上下に合わせ、それ等の端部の所定位置をボ
ルト44(44a、44b)、ナット46(46a、4
6b)等を用いて一体に結合して形成する。因みに、上
下板40、42は接着して結合してもよい。
Embodiments of the present invention will be described below with reference to the accompanying drawings. FIG. 1 is a longitudinal sectional view showing an air probe pin board before measurement of an in-circuit tester to which the present invention is applied, and FIG. 2 is an enlarged view corresponding to a circle surrounded by a chain line.
In the figure, 24 is a pin board, 26 (26a, 26b, 26
c) is the air probe, and 28 is a resin support on which the air probe 26 is erected. Each of these air probes 26 is formed into a metal elongated rod-like body, a large-diameter portion 30 is formed at the front end and a small-diameter portion 32 is formed at the rear end, and the rear end has a thickness substantially equal to the diameter of the large-diameter portion 30. Is provided. Moreover, the end 36 of the large diameter portion 30 is formed in a conical shape, and the stepped portion 38 between the large diameter portion 30 and the small diameter portion 32 is chamfered to form a truncated cone. A lead wire (not shown) is connected to the stopper 34. In this manner, when each air probe 26 is formed into an elongated rod-like body, the tips can be brought close to each other, so that a fine pitch can be handled. The support 28 is composed of two rectangular flat plates 4.
0 and 42 are aligned up and down, and the predetermined positions of the ends are bolts 44 (44a and 44b) and nuts 46 (46a and 4a).
6b) and the like to form a single body. Incidentally, the upper and lower plates 40 and 42 may be bonded and bonded.

【0011】そして、上板40には中央部の所定位置に
各エアプローブ26の大径部30が嵌まる上下に貫通し
た大径部挿通孔48と、外部の配管が連結する上下に貫
通した配管連結孔50をそれぞれ設けたものを用いる。
又、下板42には中央部の上面に広く、板厚のほぼ半分
に達する均一深さの空気室の主要部を形成する空気溜め
用の凹所52と、その凹所52の所定位置に各エアプロ
ーブ26の小径部32が嵌まる上下に貫通した小径部挿
通孔54とをそれぞれ設けたものを用いる。しかも、大
径部挿通孔48はエアプローブ26の大径部30より僅
かに径を大きくし、小径部挿通孔54はエアプローブ2
6の小径部32より僅かに径を大きくする。すると、図
2に示すように挿通孔48の内壁と大径部30との間及
び挿通孔54の内壁と小径部32との間に、Δr例えば
10〜50μmの隙間をそれぞれ形成することができ
る。なお、56(56a、56b)は上下板40、42
の位置を正確に合わせるためのノックピンである。
In the upper plate 40, a large-diameter portion insertion hole 48 which penetrates vertically into which the large-diameter portion 30 of each air probe 26 fits at a predetermined position in the center, and penetrates vertically to connect an external pipe. The one provided with each of the pipe connection holes 50 is used.
Further, the lower plate 42 has a recess 52 for an air reservoir which forms a main portion of an air chamber having a uniform depth reaching almost half of the plate thickness, which is wide on the upper surface of the central portion, and is provided at a predetermined position of the recess 52. Each air probe 26 is provided with a small-diameter portion insertion hole 54 vertically penetrated with the small-diameter portion 32 fitted therein. Moreover, the large-diameter portion insertion hole 48 has a slightly larger diameter than the large-diameter portion 30 of the air probe 26, and the small-diameter portion insertion hole 54 has the air probe 2.
6 is slightly larger in diameter than the small diameter portion 32. Then, as shown in FIG. 2, a gap of Δr, for example, 10 to 50 μm can be formed between the inner wall of the insertion hole 48 and the large diameter portion 30 and between the inner wall of the insertion hole 54 and the small diameter portion 32. . 56 (56a, 56b) is the upper and lower plates 40, 42
This is a dowel pin for accurately adjusting the position of.

【0012】このようにして、上下板40、42を一体
に結合した支持体28の所定位置に各エアプローブ26
をそれぞれ装着してピンボード24を構成すると、支持
体28の内部に各エアプローブ26の中間部を収納する
3本のエアプローブ26に共通の配管連結孔50を有す
る空気室52ができる(空気室にも空気溜め用凹所と同
一番号を付す)。そこで、ピンボード24の配管連結孔
50に図3に示すような給、排気配管路を接続する。図
中、58は配管連結孔50と結合する配管の連結部、6
0は圧縮空気源、62は真空源、64はその圧縮空気源
60からの配管路と真空源62からの配管路とを切り換
える3ポート電磁弁、66、68はその圧縮空気源60
から3ポート電磁弁64に至る配管路に介在する減圧
弁、速度制御弁である。
In this manner, each air probe 26 is positioned at a predetermined position on the support 28 in which the upper and lower plates 40 and 42 are integrally connected.
Are mounted to form the pin board 24, and an air chamber 52 having a pipe connection hole 50 common to the three air probes 26 accommodating an intermediate portion of each air probe 26 is formed in the support 28 (air). The chamber is also given the same number as the air pocket recess). Therefore, the supply and exhaust piping as shown in FIG. 3 is connected to the piping connection hole 50 of the pin board 24. In the figure, reference numeral 58 denotes a pipe connection portion connected to the pipe connection hole 50;
0 is a compressed air source, 62 is a vacuum source, 64 is a three-port solenoid valve that switches between the piping from the compressed air source 60 and the piping from the vacuum source 62, and 66 and 68 are the compressed air sources 60.
, A pressure reducing valve and a speed control valve interposed in a pipe line from the to the three-port solenoid valve 64.

【0013】測定に際してはピンボード24に対し、先
ず被検査基板70を各エアプローブ26の突出方向に少
し離して設置し、いずれの方向にも動かないように固定
する。そして、3ポート電磁弁64に通電する。する
と、電磁弁64が図3の位置から切り換わり、圧縮空気
が配管から連結孔50を通じて空気室52の内部に供給
される。室内に充満すると、円錐台状段付部38の斜面
に圧縮空気圧が作用し、各エアプローブ26の大径部3
0、小径部32が対応する挿通孔48、54の内部をそ
れぞれ先端方向に素早く突出を開始する。一旦、突出を
開始すると圧縮空気圧は大径部30の断面積から小径部
32の断面積を除いた面積に直接作用する。しかも、プ
ローブ26は内壁との隙間から空気が大気側に洩れ非接
触状態となっているので、摺動抵抗は空気層のせん断抵
抗となり、無視できる程度の微小な値となる。
At the time of measurement, first, the substrate to be inspected 70 is set slightly apart from the pin board 24 in the direction in which the air probes 26 protrude, and fixed so as not to move in any direction. Then, the three-port solenoid valve 64 is energized. Then, the electromagnetic valve 64 is switched from the position shown in FIG. 3, and compressed air is supplied from the pipe through the connection hole 50 into the air chamber 52. When the room is filled, compressed air pressure acts on the slope of the frustoconical stepped portion 38, and the large-diameter portion 3 of each air probe 26.
0, the small-diameter portion 32 quickly starts to project in the corresponding insertion holes 48, 54 toward the distal end. Once the projection starts, the compressed air pressure acts directly on the area obtained by removing the cross-sectional area of the large-diameter portion 30 from the cross-sectional area of the small-diameter portion 32. In addition, since the probe 26 is in a non-contact state in which air leaks from the gap with the inner wall to the atmosphere side, the sliding resistance becomes the shear resistance of the air layer and has a negligible small value.

【0014】すると、図4に示すように各エアプローブ
26の先端を基板70上の測定点にそれぞれ接触でき
る。その際、測定点がパターンや半田付け箇所等で凹凸
があり、各エアプローブ26のストローク(突出量)が
変わっても、接触圧(静圧)は供給する圧縮空気圧によ
り定まるため、圧縮空気圧が一定だと接触圧が一定にな
る。それ故、接触抵抗も一定になり、測定点の凹凸が測
定結果に影響を与えない。なお、減圧弁66を制御する
と、圧縮空気圧を変えて接触圧を調節できる。又、各エ
アプローブ26の先端が基板70の測定点に衝突する衝
突圧(動圧)は圧縮空気の流量により定まる。それ上、
速度制御弁68を制御すると、圧縮空気の流量を変えて
衝突圧を調節できる。なお、被検査基板70がない状態
で各エアプローブ26が突出しても、その最大ストロー
クは図5に示すように後端に備えたストッパー34の位
置により定まり、支持体28より抜けない。
Then, as shown in FIG. 4, the tip of each air probe 26 can be brought into contact with a measurement point on the substrate 70. At this time, even if the measurement point has irregularities in the pattern or the soldering position and the stroke (projection amount) of each air probe 26 changes, the contact pressure (static pressure) is determined by the supplied compressed air pressure. If it is constant, the contact pressure will be constant. Therefore, the contact resistance is also constant, and the unevenness of the measurement point does not affect the measurement result. When the pressure reducing valve 66 is controlled, the contact pressure can be adjusted by changing the compressed air pressure. The collision pressure (dynamic pressure) at which the tip of each air probe 26 collides with the measurement point of the substrate 70 is determined by the flow rate of the compressed air. Besides,
By controlling the speed control valve 68, the collision pressure can be adjusted by changing the flow rate of the compressed air. Even if each air probe 26 projects without the substrate 70 to be inspected, its maximum stroke is determined by the position of the stopper 34 provided at the rear end as shown in FIG.

【0015】測定終了後、電磁弁64への通電を切る
と、電磁弁64が図3の位置に戻って真空源62が配管
を介し、ピンボード24の連結孔50に接続されるた
め、空気室52から連結孔50を通じ、配管を経て排気
できる。すると、空気室54内の圧力が大気圧より低く
なるため各エアプローブ26の段付部38の斜面が吸引
される等して、図1の位置まで素早く後退する。なお、
エアプローブ26の測定点に対する1回の衝突でフラッ
クス膜が突き破れない場合は、電磁弁64への通電のオ
ンオフを繰り返し、何回か衝突させることにより良好な
電気的接触を得る。
When the energization of the solenoid valve 64 is stopped after the measurement, the solenoid valve 64 returns to the position shown in FIG. 3 and the vacuum source 62 is connected to the connection hole 50 of the pin board 24 via a pipe. Air can be exhausted from the chamber 52 through the connection hole 50 and the piping. Then, since the pressure in the air chamber 54 becomes lower than the atmospheric pressure, the slope of the stepped portion 38 of each air probe 26 is sucked or the like, so that the air probe 26 quickly retreats to the position shown in FIG. In addition,
If the flux film is not broken through by a single collision with the measurement point of the air probe 26, the electric power to the solenoid valve 64 is repeatedly turned on and off, and good electrical contact is obtained by colliding several times.

【0016】図6は本発明を適用したインサーキットテ
スタの測定前の他のエアプローブピンボードを示す縦断
面図である。図中、72はピンボード、74(74a、
74b、74c)はそのエアプローブ、76はそれ等の
エアプローブ74を中央部の所定位置に立設した上下板
78、80からなる樹脂製の支持体である。このピンボ
ード72は上記実施例のピンボード24と比べ、支持体
76の内部に各エアプローブ74の中間部をそれぞれ収
納する空気室82(82a、82b、82c)を設け、
それ等の空気室82を配管連結孔84付きの空気分配孔
86を介して連結する点が異なる。しかし、その他の構
造はほぼ等しい。
FIG. 6 is a longitudinal sectional view showing another air probe pin board before measurement of the in-circuit tester to which the present invention is applied. In the figure, 72 is a pin board, 74 (74a,
Reference numerals 74b and 74c) denote air probes, and reference numeral 76 denotes a resin support made of upper and lower plates 78 and 80 in which the air probes 74 are erected at predetermined positions in the center. The pin board 72 is provided with air chambers 82 (82a, 82b, 82c) for accommodating intermediate portions of the respective air probes 74 inside the support 76, as compared with the pin board 24 of the above embodiment.
The difference is that these air chambers 82 are connected via an air distribution hole 86 having a pipe connection hole 84. However, other structures are almost the same.

【0017】図7はそのような支持体76を構成する上
板78の中央部88を示す平面図、図8は図7のX−X
断面図である。この上板78は上記実施例の上板40と
同一構造を備えている。図中、90(90a、…90
h)は各エアプローブ74の大径部92が挿通する大径
部挿通孔である。因みに、大径部挿通孔90(90d、
…90h)にはそれぞれ対応する同様の各エアプローブ
74(74d、…74h)の大径部92が挿通する。但
し、エアプローブ74(74d、…74h)は図示して
いない。
FIG. 7 is a plan view showing a central portion 88 of an upper plate 78 constituting such a support 76, and FIG.
It is sectional drawing. The upper plate 78 has the same structure as the upper plate 40 of the above embodiment. In the figure, 90 (90a,... 90)
h) is a large diameter portion insertion hole through which the large diameter portion 92 of each air probe 74 is inserted. Incidentally, the large-diameter portion insertion hole 90 (90d,
90h), the corresponding large diameter portions 92 of the corresponding air probes 74 (74d,... 74h) are inserted. However, the air probe 74 (74d,... 74h) is not shown.

【0018】図9はそのような支持体76を構成する下
板80の中央部94を示す平面図、図10は図9のY−
Y断面図である。この下板80は上記実施例の下板42
と異なる構造を備えている。図中、96(96a、…9
6h)は各エアプローブ74の小径部98が挿通する小
径部挿通孔、100が下板80の上面の配管連結孔84
と同一位置に設けた空気中継用の凹所である。この空気
中継用凹所100は配管連結孔84と、空気分配孔86
(86a、86b)の主要部となる空気分配溝とをつな
ぐ部分であり、各空気分配溝86より円形状に広くする
(空気分配溝にも空気分配孔と同一番号を付す)。因み
に、小径部挿通孔96(96d、…96h)にはそれぞ
れ対応する各エアプローブ74(74d、…74h)の
小径部98が挿通し、空気室82(82d、…82h)
にはそれぞれ対応する各エアプローブ74(74d、…
74h)の中間部を収納する。又、空気分配孔86aは
3個の空気室82(82a、82b、82c)を連結
し、空気分配孔86bは5個の空気室82(82d、…
82h)を連結する。
FIG. 9 is a plan view showing the central portion 94 of the lower plate 80 constituting such a support 76, and FIG.
It is a Y sectional view. The lower plate 80 is the lower plate 42 of the above embodiment.
With a different structure. In the figure, 96 (96a,... 9)
6h) is a small diameter part insertion hole through which the small diameter part 98 of each air probe 74 is inserted, and 100 is a pipe connection hole 84 on the upper surface of the lower plate 80.
This is a recess for air relay provided at the same position as that of FIG. The air relay recess 100 has a pipe connection hole 84 and an air distribution hole 86.
(86a, 86b) is a portion connecting the air distribution grooves, which are the main parts, and is made wider in a circular shape than each air distribution groove 86 (the air distribution grooves are also given the same numbers as the air distribution holes). Incidentally, the small-diameter portions 98 of the corresponding air probes 74 (74d,... 74h) are inserted into the small-diameter portion insertion holes 96 (96d,... 96h), and the air chambers 82 (82d,.
Correspond to the respective air probes 74 (74d,...).
74h) is stored. The air distribution holes 86a connect the three air chambers 82 (82a, 82b, 82c), and the air distribution holes 86b are connected to the five air chambers 82 (82d,...).
82h).

【0019】このように、支持体76の内部に各エアプ
ローブ74の中間部をそれぞれ収納する空気室82を設
け、それ等の空気室82を配管連結孔84付きの空気中
継用凹所100を有する空気分配孔86を介して連結す
ると、圧縮空気圧が作用する面積が各空気室82、各空
気分配孔86、空気中継用凹所100の内面となって小
さくなり、機械的強度が大きくなる。それ故、支持体7
6の下板80が圧縮空気圧に耐え易くなる。
As described above, the air chambers 82 for accommodating the intermediate portions of the respective air probes 74 are provided inside the support 76, and the air chambers 82 are formed with the air relay recesses 100 having the pipe connection holes 84. When the connection is made via the air distribution holes 86 provided, the area on which the compressed air pressure acts is reduced by the inner surface of each air chamber 82, each air distribution hole 86, and the air relay recess 100, and the mechanical strength is increased. Therefore, the support 7
6 lower plate 80 can easily withstand the compressed air pressure.

【0020】[0020]

【発明の効果】以上説明した本発明によれば、請求項1
記載の発明では複数の各エアプローブの大径部と小径部
との間に形成した円錐台状段付部の斜面に圧縮空気圧を
作用させ、円滑な摺動により素早く突出させて、各エア
プローブの先端を基板上の測定点にそれぞれ接触でき
る。又、排気によって突出した各エアプローブの円錐台
状段付部の斜面に吸引作用が及ぶため、各エアプローブ
を素早く後退させることができる。それ故、検査時間を
短縮化できる。しかも、各エアプローブを細長い棒状体
にすると、先端同士を互いに至近距離に近付けることが
でき、微細の測定間ピッチに対応可能になる。又、エア
プローブの測定点に対する1回の衝突でフラックス膜が
破れない場合は、圧縮空気の供給と排気を繰り返すこと
により、何回か衝突させるとフラックス膜が破れるた
め、良好な電気的接触が得られる。又、各エアプローブ
の接触圧は測定点の凹凸に基づくストロークに関係な
く、供給する圧縮空気圧により定まるため、圧縮空気圧
を一定にすると、各エアプローブの接触抵抗も一定にな
り、正確な測定結果が得られる。
According to the present invention described above, claim 1
In the described invention, compressed air pressure is applied to the slope of the truncated conical stepped portion formed between the large diameter portion and the small diameter portion of each of the plurality of air probes, and the air probe is quickly protruded by smooth sliding. Can contact the measurement points on the substrate. Further, since the suction action is exerted on the slope of the truncated conical step portion of each air probe protruded by the exhaust, each air probe can be quickly retracted. Therefore, the inspection time can be reduced. Moreover, when each air probe is formed into a long and thin rod-like body, the tips can be brought close to each other at a close distance, and a fine pitch between measurements can be handled. If the flux film is not broken by a single collision with the air probe at the measurement point, the supply and exhaust of compressed air are repeated. can get. Also, since the contact pressure of each air probe is determined by the supplied compressed air pressure, regardless of the stroke based on the unevenness of the measurement point, if the compressed air pressure is constant, the contact resistance of each air probe will also be constant, and accurate measurement results Is obtained.

【0021】又、請求項2記載の発明では圧縮空気圧が
作用する面積が小さくなるため、機械的強度が大きく、
支持体が圧縮空気圧に耐え易くなるので、そのエアプロ
ーブ立設面の面積を大きくすることができる。
In the second aspect of the present invention, the area on which the compressed air pressure acts is small, so that the mechanical strength is large.
Since the support can easily withstand the compressed air pressure, the area of the air probe standing surface can be increased.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明を適用したインサーキットテスタの測定
前のエアプローブピンボードを示す縦断面図である。
FIG. 1 is a longitudinal sectional view showing an air probe pin board before measurement of an in-circuit tester to which the present invention is applied.

【図2】図1の一点鎖線円内に対応する拡大図である。FIG. 2 is an enlarged view corresponding to the inside of a dashed-dotted circle in FIG. 1;

【図3】同エアプローブピンボードの配管連結孔に接続
する給、排気配管路を示す図である。
FIG. 3 is a view showing supply and exhaust pipe paths connected to pipe connection holes of the air probe pin board.

【図4】同インサーキットテスタの測定時のエアプロー
ブピンボードを示す縦断面図である。
FIG. 4 is a longitudinal sectional view showing the air probe pin board at the time of measurement by the in-circuit tester.

【図5】同エアプローブピンボードの被検査基板非設置
時におけるプローブ最大突出状態を示す縦断面図であ
る。
FIG. 5 is a vertical cross-sectional view showing a state in which the probe of the air probe pin board projects maximum when the substrate to be inspected is not installed.

【図6】本発明を適用したインサーキットテスタの測定
前の他のエアプローブピンボードを示す縦断面図であ
る。
FIG. 6 is a longitudinal sectional view showing another air probe pin board before measurement of the in-circuit tester to which the present invention is applied.

【図7】同エアプローブピンボードの支持体を構成する
上板の中央部を示す平面図である。
FIG. 7 is a plan view showing a central portion of an upper plate constituting a support of the air probe pin board.

【図8】図7のX−X断面図である。FIG. 8 is a sectional view taken along line XX of FIG. 7;

【図9】同エアプローブピンボードの支持体を構成する
下板の中央部を示す平面図である。
FIG. 9 is a plan view showing a center portion of a lower plate constituting a support of the air probe pin board.

【図10】図9のY−Y断面図である。FIG. 10 is a sectional view taken along the line YY of FIG. 9;

【図11】従来のインサーキットテスタの測定時のプロ
ーブピンボードを示す縦断面図である。
FIG. 11 is a longitudinal sectional view showing a probe pin board at the time of measurement by a conventional in-circuit tester.

【符号の説明】[Explanation of symbols]

24、72…エアプローブピンボード 26、74…エ
アプローブ 28、76…支持体 30、92…大径部
32、98…小径部 34…ストッパー 38…段付
部 40、78…上板 42、80…下板 48、90
…大径部挿通孔 50、84…配管連結孔 52、82…空気室 54、
96…小径部挿通孔 58…配管の連結部 60…圧縮
空気源 62…真空源 64…3ポート電磁弁 66…減圧弁 68…速度制御弁 70…被検査基板
86…空気分配孔 100…空気中継用凹所
24, 72 ... air probe pin board 26, 74 ... air probe 28, 76 ... support body 30, 92 ... large diameter part 32, 98 ... small diameter part 34 ... stopper 38 ... stepped part 40, 78 ... upper plate 42, 80 ... Lower plate 48, 90
... large-diameter portion insertion holes 50, 84 ... pipe connection holes 52, 82 ... air chambers 54,
Reference numeral 96: small-diameter portion insertion hole 58: connection portion of piping 60: compressed air source 62: vacuum source 64: 3-port solenoid valve 66: pressure reducing valve 68: speed control valve 70: substrate to be inspected
86 ... air distribution hole 100 ... air relay recess

───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 平2−234079(JP,A) 実開 昭49−7451(JP,U) 実開 昭62−203461(JP,U) 実開 昭63−109657(JP,U) (58)調査した分野(Int.Cl.7,DB名) G01R 1/06 - 1/073 ──────────────────────────────────────────────────続 き Continuation of the front page (56) References JP-A-2-234079 (JP, A) Japanese Utility Model Showa 49-7451 (JP, U) Japanese Utility Model Showa 62-203461 (JP, U) Japanese Utility Model Showa 63- 109657 (JP, U) (58) Field surveyed (Int. Cl. 7 , DB name) G01R 1/06-1/073

Claims (2)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 複数のエアプローブを立設した支持体か
らなる基板検査装置用のエアプローブピンボードにおい
て、上記各エアプローブとして、先端側を大径部、後端
側を小径部に形成し、その大径部と小径部との間を円錐
台状の段付部に形成して、後端に小径部の径より拡大し
たストッパーを備えた細長い棒状体を用い、支持体の内
部に各エアプローブの中間部を収納する複数のエアプロ
ーブに共通の配管連結孔付き空気室を設け、その空気室
で分けられた支持体の一方の側部分に各エアプローブの
大径部より僅かに大きな径を有する大径部挿通孔をそれ
ぞれ設け、他方の側部分に各エアプローブの小径部より
僅かに大きな径を有する小径部挿通孔をそれぞれ設ける
ことを特徴とする基板検査装置用のエアプローブピンボ
ード。
1. An air probe pin board for a board inspection device comprising a support having a plurality of air probes erected thereon, wherein each of said air probes has a large diameter portion at the front end and a small diameter portion at the rear end. Between the large-diameter portion and the small-diameter portion to form a truncated cone-shaped stepped portion, using a long and narrow rod-shaped body provided with a stopper larger than the diameter of the small-diameter portion at the rear end, each inside the support A plurality of air probes accommodating an intermediate portion of the air probe are provided with an air chamber having a common pipe connection hole, and one side portion of the support divided by the air chamber is slightly larger than a large diameter portion of each air probe. An air probe pin for a board inspection device, wherein a large-diameter portion insertion hole having a diameter is provided, and a small-diameter portion insertion hole having a diameter slightly larger than the small diameter portion of each air probe is provided on the other side portion. board.
【請求項2】 複数のエアプローブを立設した支持体か
らなる基板検査装置用のエアプローブピンボードにおい
て、上記各エアプローブとして、先端側を大径部、後端
側を小径部に形成し、その大径部と小径部との間を円錐
台状の段付部に形成して、後端に小径部の径より拡大し
たストッパーを備えた細長い棒状体を用い、支持体の内
部に各エアプローブの中間部をそれぞれ収納する空気室
を設け、それ等の空気室を配管連結孔付き空気分配孔を
介して連結し、それ等の空気室で分けられた支持体の一
方の側部分に各エアプローブの大径部より僅かに大きな
径を有する大径部挿通孔をそれぞれ設け、他方の側部分
に各エアプローブの小径部より僅かに大きな径を有する
小径部挿通孔をそれぞれ設けることを特徴とする基板検
査装置用のエアプローブピンボード。
2. An air probe pin board for a board inspection device comprising a support having a plurality of air probes erected thereon, wherein each of the air probes has a large-diameter portion at the front end and a small-diameter portion at the rear end. Between the large-diameter portion and the small-diameter portion to form a truncated cone-shaped stepped portion, using a long and narrow rod-shaped body provided with a stopper larger than the diameter of the small-diameter portion at the rear end, each inside the support Air chambers for accommodating the intermediate portions of the air probes are provided, and these air chambers are connected via air distribution holes with pipe connection holes, and are provided on one side of the support divided by the air chambers. It is necessary to provide a large-diameter portion insertion hole having a diameter slightly larger than the large-diameter portion of each air probe, and to provide a small-diameter portion insertion hole having a diameter slightly larger than the small-diameter portion of each air probe on the other side portion. Features air pro for board inspection equipment Bubpin board.
JP16425293A 1993-06-08 1993-06-08 Air probe pin board for board inspection equipment Expired - Fee Related JP3308346B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16425293A JP3308346B2 (en) 1993-06-08 1993-06-08 Air probe pin board for board inspection equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16425293A JP3308346B2 (en) 1993-06-08 1993-06-08 Air probe pin board for board inspection equipment

Publications (2)

Publication Number Publication Date
JPH06347477A JPH06347477A (en) 1994-12-22
JP3308346B2 true JP3308346B2 (en) 2002-07-29

Family

ID=15789573

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16425293A Expired - Fee Related JP3308346B2 (en) 1993-06-08 1993-06-08 Air probe pin board for board inspection equipment

Country Status (1)

Country Link
JP (1) JP3308346B2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7762822B2 (en) 2005-04-27 2010-07-27 Aehr Test Systems Apparatus for testing electronic devices
KR100911660B1 (en) * 2007-07-11 2009-08-10 (주)엠투엔 Probe substrate assembly of probe card and probe card using same
US8030957B2 (en) 2009-03-25 2011-10-04 Aehr Test Systems System for testing an integrated circuit of a device and its method of use
US10466292B2 (en) 2016-01-08 2019-11-05 Aehr Test Systems Method and system for thermal control of devices in an electronics tester
CN110383092B (en) 2017-03-03 2022-04-01 雅赫测试系统公司 Electronic tester
EP4226165A1 (en) 2020-10-07 2023-08-16 AEHR Test Systems Electronics tester

Also Published As

Publication number Publication date
JPH06347477A (en) 1994-12-22

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